Bearing assemblies, apparatuses, and motor assemblies using the same

ABSTRACT

Bearing assemblies, apparatuses, and motor assemblies using the same are disclosed. In an embodiment, a bearing assembly may include a plurality of superhard bearing elements distributed circumferentially about an axis. Each of the superhard bearing elements may include a bearing surface. The bearing assembly may also include a support ring structure having a support ring that carries the superhard bearing elements. The support ring structure may include at least one erosion resistant region exhibiting a higher erosion resistance than another region of the support ring.

CROSS-REFERENCE TO RELATED APPLICATIONS

This application is a continuation of U.S. application Ser. No.14/856,210 filed 16 Sep. 2015, which is a continuation of U.S.application Ser. No. 13/736,474 filed on 8 Jan. 2013 (now U.S. Pat. No.9,163,660 issued on 20 Oct. 2015). The disclosure of each of theforegoing applications is incorporated herein, in its entirety, by thisreference.

BACKGROUND

Subterranean drilling systems that employ downhole drilling motors arecommonly used for drilling boreholes in the earth for oil and gasexploration and production. Such subterranean drilling systems typicallyinclude a downhole drilling motor that is operably connected to anoutput shaft. A pair of thrust-bearing apparatuses also can be operablycoupled to the downhole drilling motor. A rotary drill bit configured toengage a subterranean formation and drill a borehole can be connected tothe output shaft. As the borehole is drilled with the rotary drill bit,pipe sections may be connected to the subterranean drilling system toform a drill string capable of progressively drilling the borehole to agreater size or depth within the earth.

Each thrust-bearing apparatus includes a stator that does not rotaterelative to the motor housing and a rotor that is attached to the outputshaft and rotates with the output shaft. The stator and rotor eachincludes a plurality of bearing elements that may be fabricated frompolycrystalline diamond compacts (“PDCs”) that provide diamond bearingsurfaces that bear against each other during use.

In operation, high-pressure drilling fluid may be circulated through thedrill string and power section of the downhole drilling motor, usuallyprior to the rotary drill bit engaging the bottom of the borehole, togenerate torque and rotate the output shaft and the rotary drill bitattached to the output shaft. When the rotary drill bit engages thebottom of the borehole, a thrust load is generated, which is commonlyreferred to as “on-bottom thrust” that tends to compress and is carried,at least in part, by one of the thrust-bearing apparatuses. Fluid flowthrough the power section may cause what is commonly referred to as“off-bottom thrust,” which is carried, at least in part, by the otherthrust-bearing apparatus. The on-bottom and off-bottom thrust carried bythe thrust-bearing apparatuses can also be extremely large and generatesignificant amounts of energy.

The operational lifetime of the bearing apparatuses often can determinethe useful life of the subterranean drilling system. Therefore,manufacturers and users of bearing apparatuses continue to attempt toimprove their operational lifetime.

SUMMARY

Various embodiments of the invention relate to bearing assemblies,apparatuses, and motor assemblies that include superhard bearingelements carried by a support ring structure that includes at least oneerosion resistant region exhibiting a higher erosion resistant thananother region of an underlying support ring. Such bearing assembliesmay be employed in bearing apparatuses for use in downhole motors of asubterranean drilling system or other mechanical systems.

In an embodiment, a bearing assembly may include a plurality ofsuperhard bearing elements distributed circumferentially about an axis.Each of the plurality of superhard bearing elements includes a superhardbearing surface. A support ring structure including a support ringcarries the plurality of superhard bearing elements. The support ringstructure further includes at least one erosion resistant regionexhibiting a higher erosion resistance than another region of thesupport ring.

In an embodiment, a bearing apparatus may include a first bearingassembly including a plurality of superhard bearing elements distributedcircumferentially about an axis. Each of the plurality of superhardbearing elements in the first bearing assembly includes a firstsuperhard bearing surface. A support ring structure including a supportring carries the plurality of superhard bearing elements within thefirst bearing assembly. The support ring structure may include at leastone erosion resistant region exhibiting a higher erosion resistance thananother region of the support ring. The bearing apparatus also includesa second bearing assembly including a plurality of second superhardbearing elements, each of the second superhard bearing elementsincluding a second superhard bearing surface oriented to engage thefirst superhard bearing surfaces of the first bearing assembly duringoperation of the bearing apparatus. The bearing apparatus also includesa second support ring that carries the plurality of second superhardbearing elements.

In an embodiment, a method of operating a bearing apparatus may includerotating a first bearing assembly relative to a second bearing assembly,wherein at least one of the first or second bearing assemblies includesa plurality of superhard bearing elements distributed circumferentiallyabout an axis, with each of the plurality of superhard bearing elementsincluding a superhard bearing surface. A support ring structure isprovided, which includes a support ring that carries the plurality ofsuperhard bearing elements. The support ring may include at least oneerosion resistant region exhibiting a higher erosion resistance thananother region of the support ring.

In an embodiment, a method of fabricating a bearing assembly may includeproviding a support ring and machining the support ring to include aplurality of recesses for receiving a plurality of superhard bearingelements. The plurality of recesses is distributed circumferentiallyabout an axis. The method also includes depositing an erosion resistantcoating onto at least a portion of a surface of the support ring betweeneach of the plurality of recesses, and mounting each of the plurality ofsuperhard bearing elements in a corresponding one of the plurality ofrecesses in the support ring.

Other embodiments include downhole motors for use in drilling systemsand subterranean drilling systems that may utilize any of the disclosedbearing apparatuses.

Features from any of the disclosed embodiments may be used incombination with one another, without limitation. In addition, otherfeatures and advantages of the present disclosure will become apparentto those of ordinary skill in the art through consideration of thefollowing detailed description and the accompanying drawings.

BRIEF DESCRIPTION OF THE DRAWINGS

The drawings illustrate several embodiments, wherein identical referencenumerals refer to identical or similar elements or features in differentviews or embodiments shown in the drawings.

FIG. 1A is an isometric view of a thrust-bearing assembly according toan embodiment;

FIG. 1B is a top plan view of the thrust-bearing assembly shown in FIG.1A;

FIG. 1C is an isometric cutaway view taken along line 1C-1C of thethrust-bearing assembly shown in FIG. 1B;

FIG. 2A is a top plan view of a thrust-bearing assembly according to anembodiment;

FIG. 2B is an isometric cutaway view taken along line 2B-2B of thethrust-bearing assembly shown in FIG. 2A.

FIG. 3A is an exploded isometric cutaway view of a radial bearingapparatus according to an embodiment.

FIG. 3B is an isometric view of the outer radial bearing assembly shownin FIG. 3A.

FIG. 3C is an isometric cutaway view of the outer radial bearingassembly taken along line 3C-3C of the radial bearing assembly shown inFIGS. 3A and 3B.

FIG. 4A is an isometric view of a thrust-bearing assembly according toan embodiment;

FIG. 4B is a top plan view of the thrust-bearing assembly shown in FIG.4A according to an embodiment;

FIG. 4C is an isometric cutaway view taken along line 4C-4C of thethrust bearing assembly shown in FIG. 4B;

FIG. 4D is a partial isometric cutaway view of the thrust-bearingassembly shown in FIGS. 4A-4C according to an embodiment;

FIG. 4E is an isometric view of one of the inserts shown in FIGS. 4A-4D,according to an embodiment;

FIG. 5A is a partial isometric cutaway view of a thrust-bearing assemblyaccording to an embodiment;

FIG. 5B is an isometric view of an insert of the thrust-bearing assemblyshown in FIG. 5A according to an embodiment;

FIG. 6A is a partial isometric cutaway view of a thrust-bearing assemblyaccording to an embodiment;

FIG. 6B is an isometric view of an insert of the thrust-bearing assemblyshown in FIG. 6A according to an embodiment;

FIG. 7A is an isometric view of a thrust-bearing apparatus that mayemploy any of the disclosed thrust-bearing assemblies according to anembodiment;

FIG. 7B is a cross-sectional view of the thrust-bearing apparatus shownin FIG. 7A take along line 7B-7B;

FIG. 8A is an exploded isometric view of a radial bearing apparatusincluding a cutaway view of an inner radial bearing assembly accordingto an embodiment;

FIG. 8B is an isometric view of the outer radial bearing assembly shownin FIG. 8A;

FIG. 8C is an isometric cutaway view of the outer radial bearingassembly taken along line 8C-8C of the radial bearing assembly shown inFIGS. 8A and 8B;

FIGS. 8D and 8E are isometric views of the outer radial bearing assemblyand an insert, respectively, shown in FIGS. 8A-8C, according to anembodiment;

FIG. 9A is an isometric view of a thrust-bearing assembly according toan embodiment;

FIGS. 9B and 9C are isometric views of the thrust-bearing assembly andan insert, respectively, shown in FIG. 9A, according to an embodiment;

FIG. 9D is a top plan view illustrating the beginning stage ofmanufacture of the superhard bearing elements and erosion resistantregions shown in FIGS. 9A-9C according to an embodiment;

FIG. 9E is a side elevation view of the superhard bearing element anderosion resistant regions shown in FIGS. 9A-9D;

FIG. 10 is an isometric view of a radial bearing assembly according toan embodiment; and

FIG. 11 is a schematic isometric cutaway view of a subterranean drillingsystem including a thrust-bearing apparatus utilizing any of thedisclosed bearing assemblies according to various embodiments.

DETAILED DESCRIPTION

Various embodiments of the invention relate to bearing assemblies,apparatuses, and motor assemblies that include superhard bearingelements carried by a support ring structure that includes at least oneerosion resistant region exhibiting a higher erosion resistance thananother region of an underlying support ring. The disclosed bearingapparatuses, methods of using bearing apparatuses, and motor assembliesmay be used in a variety of applications, such as drilling equipment,machining equipment, pumps, bearing apparatuses, and other articles.

FIGS. 1A and 1B are isometric and top plan views, respectively, of athrust-bearing assembly 100 according to an embodiment. Thethrust-bearing assembly 100 may form a stator or a rotor of athrust-bearing apparatus used in a subterranean drilling system. Thethrust-bearing assembly 100 may include a support ring structure 101having a support ring 102 defining an opening 104 through which a shaft(not shown) of, for example, a downhole drilling motor may extend. Thesupport ring 102 may be made from a variety of different materials. Forexample, the support ring 102 may comprise a metal, alloy steel, a metalalloy, carbon steel, stainless steel, tungsten carbide, combinations ofthe foregoing, or any other suitable metal or conductive ornon-conductive material.

The support ring structure 101 further includes a plurality of erosionresistant regions including an erosion resistant coating 106 that atleast partially covers one or more surfaces of the support ring 102.Such erosion resistant regions/coating 106 may provide erosionprotection of the support ring 102 from abrasive drilling fluid/mudduring operation of the thrust bearing assembly 100. The erosionresistant coating 106 may include an erosion resistant materialexhibiting a higher erosion resistance than the support ring 102. Forexample, the erosion resistant coating 106 may comprise a carbide, asuperhard material, a metal carbide (e.g., tungsten carbide, niobiumcarbide, molybdenum carbide, vanadium carbide, titanium carbide, orcombinations thereof), a cemented carbide (e.g., tungsten carbide,niobium carbide, molybdenum carbide, silicon carbide, boron nitride,boron, carbide, vanadium carbide, titanium carbide, or combinationsthereof cemented with cobalt, iron, nickel, or alloys thereof), diamond,boron nitride, combinations of the foregoing, or other suitable erosionresistant material. Any suitable test method for conducting erosiontests may be used. For example, American Society for Testing andMaterials (“ASTM”) has numerous standards that may be used for erosiontesting of the erosion resistant coating 106.

The erosion resistant coating 106 may be laser-applied to the supportring 102; coated via chemical vapor deposition (“CVD”) or variantsthereof (e.g., plasma-enhanced CVD, etc., without limitation); may bepre-formed and secured to the support ring 102 via brazing, fasteningwith a fastener, welding (e.g., tungsten inert gas (“TIG”) welding,manual metal arc welding, or plasma transferred arc (“PTA”) welding),thermal spray welding, plasma spray welding, spray and fuse welding,oxy-acetylene welding, submerged arc welding, wire spray welding, manualtorch welding, powder welding, flame spray welding, electrical arcwelding, metal inert gas (“MIG”) welding, or combinations of theforegoing; or may be applied by another suitable technique. For example,a commercially available CVD tungsten carbide layer (currently marketedunder the trademark HARDIDE®) is available from Hardide Layers Inc. ofHouston, Tex. In other embodiments, the erosion resistant coating 106may be formed by physical vapor deposition (“PVD”), variants of PVD,high-velocity oxygen fuel (“HVOF”) thermal spray processes, or any othersuitable process, without limitation.

In other embodiments, hardfacing may be used to create a high-strengthmetallurgical bond between the support ring 102 and the erosionresistant coating 106, ensuring that the erosion resistant coating 106does not flake off even under high mechanical loading. For example, forextreme demands on erosion resistance and bond strength, the erosionresistant coating 106 may be hardfaced onto the support ring 102 usingTIG welding, manual metal arc welding, or PTA welding.

TIG welding involves drawing an arc between a non-consumable tungstenelectrode and the support ring 102. The electrode, the arc, and thematerial from which the erosion resistant coating 106 is formed areprotected from the atmosphere with an inert shielding gas. For manualwelding, the material from which the erosion resistant coating 106 isformed may be provided in the form of a rod. The TIG process may also bemechanized. In such case a manipulator may be used to relatively movethe support ring 102 in relation to the welding torch and the hardfacingwire or rod.

Manual metal arc welding involves drawing an arc between a consumableelectrode and the support ring 102. The erosion resistant metalliccore-wire may be melted by the arc and transferred to the weld-pool asmolten drops. The melted electrode coating may form a gas shield aroundthe arc and the weld pool as well as a slag on the surface of theweld-pool, thus shielding the cooling weld-pool from the atmosphere.Manual metal arc welding employs low cost equipment, has low operatingcosts, and the equipment relatively easy to transport.

PTA welding provides for ease of automation and a high degree ofreproducibility of the welded erosion resistant coating 106. Anadvantage of the PTA process is that the powder form of the hardfacingmaterials may allow for the fabrication of the erosion resistant coating106 from a variety of different materials and combinations of materialswith a wide range of hardness and erosion resistant properties.

The support ring 102 may include a plurality of recesses 108 (shown inFIG. 1C) formed therein, each of which receives a corresponding one ofthe superhard bearing elements 110. The superhard bearing elements 110may include a superhard table 112 bonded to a substrate 114, with asuperhard table 112 having and a bearing surface 116. In an embodiment,one or more of the superhard bearing elements 110 may have a generallycylindrical 3D shape. While the superhard bearing elements 110 are shownhaving a generally cylindrical shape, the one or more of the superhardbearing elements 110 may have any solid geometry, such as a generallycubic geometry, a generally polyhedron geometry, or any generally planegeometry that has a thickness or depth. For example, the bearing surface116 of the superhard bearing element 110 may have a generallyrectangular 2D shape, a generally oval shape, a generally wedge shape, agenerally polygonal shape, or any other suitable geometry.

The superhard bearing elements 110 are illustrated in FIGS. 1A and 1B asbeing distributed circumferentially about a thrust axis 118 along whicha thrust force may be generally directed during use. As shown, gaps 120may be located between adjacent ones of the superhard bearing elements110. In an embodiment, at least one of, some of, or all of the gaps 120may exhibit a width of about 0.00020 inches to 0.500 inches, such asabout 0.10 inches to about 0.3 inches, about 0.10 inches to about 0.4inches, about 0.00040 inches to 0.0010 inches, or about 0.00040 inchesto 0.080 inches. In other embodiments, the gaps 120 may have widths thatare relatively larger or smaller. In other embodiments, the gaps 120 mayvary between different adjacent ones of the superhard bearing elements110.

Each of the superhard bearing elements 110 may be partially disposedwithin a corresponding one of the plurality of recesses 108 of thesupport ring 102 and secured partially therein via brazing,press-fitting, threadly attaching, fastening with a fastener,combinations of the foregoing, or another suitable technique. Thesuperhard bearing elements 110 may be pre-machined to tolerances andmounted in the support ring 102 and the erosion resistant coating 106and/or mounted to the support ring 102 and the erosion resistant coating106 and the bearing surfaces 116 thereof and planarized (e.g., bylapping and/or grinding) so that the bearing surfaces 116 aresubstantially coplanar. Optionally, one or more of the superhard bearingelements 110 may exhibit a peripherally extending edge chamfer 122,shown in FIGS. 1B and 1C. However, in other embodiments, the edgechamfer may be omitted.

In an embodiment, the erosion resistant coating 106 may be depositedonly on areas of the support ring 102 prone to erosion from abrasivedrilling fluid/mud during operation of the thrust bearing assembly 100.For example, the erosion resistant coating 106 may be deposited onlybetween the superhard bearing elements 110.

In an embodiment, the superhard bearing elements 110 may be mounted tothe support ring structure 101 following deposition of the erosionresistant coating 106 onto at least a portion of a surface of thesupport ring 102. In some embodiments, the erosion resistant coating 106may even coat side and bottom surfaces of the recesses 108, while inother embodiments the side and bottom surfaces of the recesses may notbe coated.

In another embodiment, the superhard bearing elements 110 may be mountedto the support ring structure 101 prior to deposition of the erosionresistant coating 106 onto at least a portion of a surface of thesupport ring 102.

In an embodiment, the erosion resistant coating 106 may be machinedfollowing deposition on the support ring structure 104 and prior toattachment or mounting of each of the superhard bearing elements 110into a corresponding one of the plurality of recesses 108. In otherembodiments, the erosion resistant coating 106 may be machined followingdeposition and after attachment or mounting of each of the superhardbearing elements 110 into a corresponding one of the plurality ofrecesses 108. For example, the erosion resistant coating 106 may bemachined on the support ring structure 101 using milling machines, saws,grinding machines, electrical discharge machining (“EDM”),electro-chemical erosion, laser cutting, or water jet cutting to shapethe erosion resistant coating. The machining may include drilling,turning, boring, milling, laser cutting, diamond wire cutting, and wireEDM.

As used herein, a “superhard bearing element” is a bearing elementincluding a bearing surface that is made from a material exhibiting ahardness that is at least as hard as tungsten carbide. In any of theembodiments disclosed herein, the superhard bearing elements maycomprise one or more superhard materials, such as polycrystallinediamond, polycrystalline cubic boron nitride, silicon carbide, tungstencarbide, or any combination of the foregoing superhard materials. Forexample, the superhard table 112 may comprise polycrystalline diamondand the substrate 114 may comprise cobalt-cemented tungsten carbide.Furthermore, in any of the embodiments disclosed herein, thepolycrystalline diamond table may be leached to at least partiallyremove or substantially completely remove a metal-solvent catalyst(e.g., cobalt, iron, nickel, or alloys thereof) that was used toinitially sinter precursor diamond particles to form the polycrystallinediamond. In another embodiment, an infiltrant used to re-infiltrate apreformed leached polycrystalline diamond table may be leached orotherwise removed to a selected depth from a bearing surface. Moreover,in any of the embodiments disclosed herein, the polycrystalline diamondmay be un-leached and include a metal-solvent catalyst (e.g., cobalt,iron, nickel, or alloys thereof) that was used to initially sinter theprecursor diamond particles that form the polycrystalline diamond and/oran infiltrant used to re-infiltrate a preformed leached polycrystallinediamond table. Examples of methods for fabricating the superhard bearingelements and superhard materials and/or structures from which thesuperhard bearing elements can be made are disclosed in U.S. Pat. Nos.7,866,418; 7,998,573; 8,034,136; and 8,236,074; the disclosure of eachof the foregoing patents is incorporated herein, in its entirety, bythis reference.

The diamond particles that may be used to fabricate the superhard table208 in a high-pressure/high-temperature process (“HPHT)” may exhibit alarger size and at least one relatively smaller size. As used herein,the phrases “relatively larger” and “relatively smaller” refer toparticle sizes (by any suitable method) that differ by at least a factorof two (e.g., 30 μm and 15 μm). According to various embodiments, thediamond particles may include a portion exhibiting a relatively largersize (e.g., 70 μm, 60 μm, 50 μm, 40 μm, 30 μm, 20 μm, 15 μm, 12 μm, 10μm, 8 μm) and another portion exhibiting at least one relatively smallersize (e.g., 15 μm, 12 μm, 10 μm, 8 μm, 6 μm, 5 μm, 4 μm, 3 μm, 2 μm, 1μm, 0.5 μm, less than 0.5 μm, 0.1 μm, less than 0.1 μm). In anembodiment, the diamond particles may include a portion exhibiting arelatively larger size between about 10 μm and about 40 μm and anotherportion exhibiting a relatively smaller size between about 1 μm and 4μm. In another embodiment, the diamond particles may include a portionexhibiting the relatively larger size between about 15 μm and about 50μm and another portion exhibiting the relatively smaller size betweenabout 5 μm and about 15 μm. In another embodiment, the relatively largersize diamond particles may have a ratio to the relatively smaller sizediamond particles of at least 1.5. In some embodiments, the diamondparticles may comprise three or more different sizes (e.g., onerelatively larger size and two or more relatively smaller sizes),without limitation. The resulting polycrystalline diamond formed fromHPHT sintering the aforementioned diamond particles may also exhibit thesame or similar diamond grain size distributions and/or sizes as theaforementioned diamond particle distributions and particle sizes.Additionally, in any of the embodiments disclosed herein, the superhardbearing elements may be free-standing (e.g., substrateless) and formedfrom a polycrystalline diamond body that is at least partially or fullyleached to remove a metal-solvent catalyst initially used to sinter thepolycrystalline diamond body.

FIGS. 2A and 2B are top plan and isometric cutaway views of athrust-bearing assembly 200 according to an embodiment. Thethrust-bearing assembly 200 may form a stator or a rotor of athrust-bearing apparatus. The thrust-bearing assembly 200 may include asupport ring structure 201 having a support ring 202 defining an opening204 through which a shaft (not shown) of, for example, a downholedrilling motor may extend. Similar to the support ring 102, the supportring 202 may be made from a variety of different materials. For example,the support ring 202 may comprise a metal, an alloy steel, a metalalloy, carbon steel, a stainless steel, tungsten carbide, combinationsof the foregoing, or any other suitable conductive or non-conductivematerial.

The thrust-bearing assembly 200 may include a plurality of superhardbearing elements 206. The superhard bearing elements 206 may include asuperhard table 208 bonded to a substrate 210, with the superhard table208 including a bearing surface 212. Each of the plurality of superhardbearing elements 206 may comprise a superhard compact or any othersuperhard material or structure disclosed herein. In an embodiment, oneor more of the superhard bearing elements 206 may have a generalcylindrical 3D shape. While the superhard bearing elements 206 are shownhaving a generally cylindrical shape, each of the plurality of superhardbearing elements 206 may have any solid geometry such as a generallycubic geometry, a generally polyhedron geometry, or any generally planegeometry that has a thickness or depth. For example, one or more of thesuperhard bearing elements 206 may have a general rectangular shape, ageneral oval shape, or any other suitable geometry.

The thrust-bearing assembly 200 (as shown in FIGS. 2A and 2B) may haveeach of the superhard bearing elements 206 attached to the support ring202 prior to the coating of the support ring 202 with the erosionresistant coating 214. For example, following attachment of each of thesuperhard bearing elements 206 to the support ring 202, protective cupsmay be positioned over each of the superhard bearing elements 206 priorto deposition of the erosion resistant coating 214. Such protective cupsmay serve to protect and/or cool each of the superhard bearing elements206 during the erosion resistant coating deposition process.

Following deposition of the erosion resistant coating 214, theprotective cups may be removed from each of the superhard bearingelements 206. A gap 216 surrounding each of the superhard bearingelements 206 may result from the presence of the protective cup duringprocessing. As shown in FIGS. 2A and 2B, gaps 216 may be located betweenthe superhard bearing elements 206 and the erosion resistant coating214. In an embodiment, at least one of, some of, or all of the gaps 216may exhibit a width 218 (as shown in FIG. 2B) of about 0.00020 inches to0.25 inches, such as about 0.050 inches to about 0.1 inches, about 0.10inches to about 0.2 inches, about 0.00040 inches to 0.0010 inches, orabout 0.00040 inches to 0.080 inches. In other embodiments, the gaps 216may have widths 218 that are relatively larger or smaller. In otherembodiments, the gaps 216 may vary between different adjacent ones ofthe superhard bearing elements 206.

The concepts used in the thrust-bearing assemblies and apparatusesdescribed above may also be employed in radial bearing assemblies andapparatuses. For example, FIGS. 3A-3C are exploded, isometric, andisometric cutaway views, respectively, of a radial bearing apparatus 300according to an embodiment. The radial bearing apparatus 300 may includea first radial bearing assembly 302 (i.e., an inner race) and a secondradial bearing assembly 304 (i.e., an outer race). The first radialbearing assembly 302 may be configured as a rotor and may include asupport ring structure 305 including a support ring 306 and a pluralityof superhard bearing elements 308 extending about a rotation axis 310.The support ring 306 may include an inner peripheral surface defining acentral opening 312.

As shown in FIG. 3A, the support ring structure 305 includes the supportring 306 and an erosion resistant coating 314 disposed thereon that mayenhance the erosion resistance of the support ring 306. Much like theerosion resistant coating 106, the erosion resistant coating 314 maycomprise a carbide, a superhard material, a metal carbide (e.g.,tungsten carbide, niobium carbide, molybdenum carbide, vanadium carbide,titanium carbide, or combinations thereof), a cemented carbide (e.g.,tungsten carbide, niobium carbide, molybdenum carbide, boron carbide,silicon carbide, vanadium carbide, titanium carbide, or combinationsthereof cemented with cobalt, iron, nickel, or alloys thereof), diamond,boron nitride, combinations of the foregoing, or other suitable erosionresistant material. The erosion resistant coating 314 may be applied tothe support ring 306 using any of the methods disclosed herein.

As illustrated in FIG. 3A, the superhard bearing elements 308 may bedistributed circumferentially about a rotation axis 310 in a pluralityof corresponding recesses 318 formed in the support ring 306 of thesupport ring structure 305 and arranged in a single row. In otherembodiments, the superhard bearing elements 308 may be circumferentiallydistributed in two rows, three rows, four rows, or any other number ofrows. At least one, some of, or each superhard bearing element 308 mayinclude a superhard table 320 (shown in FIG. 3A) including aconvexly-curved bearing surface 322 (e.g., curved to lie on an imaginarycylindrical surface). Each superhard table 320 may be bonded or attachedto a corresponding substrate 324. The superhard bearing elements 308 mayhave a generally cylindrical shape and may be made from any of thematerials discussed above for the superhard bearing elements 110, or206. In other embodiments, the superhard bearing elements 308 may havedifferent shapes and/or sizes. For example, one or more of the superhardbearing surfaces 322 may have any solid geometry such as a generallycubic geometry, or a generally polyhedron geometry, or any generallyplane geometry that has a thickness or depth. For example, a bearingsurface of a superhard bearing element may have a generally rectangularshape, a generally elliptical shape, a generally wedge shape, agenerally polygonal shape, a generally oval shape, or any other suitablegeometry, and/or at least one of the superhard bearing elements 308 maybe sized larger than another one of the superhard bearing elements 308.

The second radial bearing assembly 304 may be configured as a statorthat extends about and receives the first radial bearing assembly 302(i.e., rotor). The second radial bearing assembly 304 may be generallyconfigured similar to the first radial bearing assembly 302 or any otherradial bearing assembly disclosed herein. For example, the second radialbearing assembly 304 may include a support ring structure 325 comprisinga support ring 326 including an erosion resistant coating 328 (FIG. 3C)formed from any of the materials disclosed herein for the erosionresistant coating 314, and a plurality of superhard bearing elements330.

The erosion resistant coating 328 may provide erosion resistance regionslaterally surrounding each of the superhard bearing elements 330. Thesuperhard bearing elements 330 may be machined to tolerances and mountedin the support ring 326 and/or attached to the support ring 326 of thesupport ring structure 325 according to any of the embodiments disclosedherein.

At least one of, some of, or each superhard bearing element 330 mayinclude a superhard table 334 (shown in FIG. 3C) including aconcavely-curved bearing surface 336 curved to correspond to theconvexly-curved bearing surfaces 322 of the superhard bearing elements308. Each of the superhard bearing elements 330 including the concavelycurved bearing surface 336 may be oriented to engage the convexly-curvedbearing surfaces 322 of the first bearing assembly 302 during operation.Similar to the superhard bearing elements 308, the superhard bearingelements 330 may have a general cylindrical shape and may be made fromany of the materials and structures discussed above for any superhardbearing elements disclosed herein.

While the superhard bearing elements 330 are shown configured similarlyto one another and the superhard bearing elements 308, in otherembodiments, the superhard bearing elements 330 may have any solidgeometry such as a generally cubic geometry, a generally polyhedrongeometry, or any generally plane geometry that has a thickness or depth.For example, the bearing surface 336 of the superhard bearing element330 may have a generally rectangular shape, a generally ellipticalshape, a generally wedge shape, a generally polygonal shape, a generallyoval shape, or any other suitable geometry. In other embodiments, atleast one of the superhard bearing elements 308 may have a generallyrectangular shape and at least one of the superhard bearing 330 elementsmay have a generally elliptical shape. In yet other embodiments, atleast one of the superhard bearing elements 330 may be sized larger thanat least one of the superhard bearing elements 308.

In an embodiment, a shaft or spindle (not shown) may extend through theopening 312 and may be secured to the first radial bearing assembly 302,threadly coupling the shaft or spindle to the first radial bearingassembly 302, or another suitable technique. A housing (not shown) mayalso be secured to the second radial bearing assembly 304 using similartechniques. While the first radial bearing assembly 302 is shownconfigured as the rotor and the second radial bearing assembly 304 isshown configured as the stator, in other embodiments, the first radialbearing assembly 302 may be configured as the stator and the secondradial bearing assembly 304 may be configured as the rotor.

FIGS. 4A and 4B are isometric and top plan views of a thrust-bearingassembly 400 according to an embodiment. The thrust-bearing assembly 400may form a stator or a rotor of a thrust-bearing apparatus. Thethrust-bearing assembly 400 may include a support ring structure 401having a support ring 402 defining an opening 404 through which a shaft(not shown) of, for example, a downhole drilling motor may extend.Similar to the support ring 102, the support ring 402 may be made from avariety of different materials. For example, the support ring 402 maycomprise a metal, an alloy steel, a metal alloy, carbon steel, astainless steel, tungsten carbide, combinations of the foregoing, or anyother suitable conductive or non-conductive material.

The superhard bearing elements 406 are illustrated in FIGS. 4A and 4Bbeing distributed circumferentially about a thrust axis 414 along whicha thrust force may be generally directed during use. As shown in FIG.4B, gaps 416 may be located between adjacent ones of the superhardbearing elements 406. In an embodiment, at least one of, some of, or allof the gaps 416 may exhibit width of about 0.00020 inches to 0.500inches, such as about 0.10 inches to about 0.3 inches, about 0.10 inchesto about 0.4 inches, about 0.00040 inches to 0.0010 inches, or about0.00040 inches to 0.080 inches. In other embodiments, the gaps 416 mayhave widths that are relatively larger or smaller. In other embodiments,one or more of the gaps 416 may have different widths. For example, onepair of adjacent ones of the superhard bearing elements 406 may becloser together than another pair of adjacent ones of the superhardbearing elements 406.

As shown in FIGS. 4C and 4D, the support ring 402 may include an annularslot 423 having a plurality of recesses 422 formed in a base surfacethereof. Each of the superhard bearing elements 406 may be disposed in acorresponding one of the plurality of recesses 422 and project from theannular slot 423.

Increased erosion resistance in lateral regions surrounding each of theplurality of superhard bearing elements 406 may provide for increasederosion resistance of the support ring 402. Abrasive-laden fluids maycause erosion of the support ring 402, which carries the plurality ofsuperhard bearing elements 406. This erosion may be caused by contactfrom abrasive particles suspended in fluid during operation. Erosion ofareas between and in close proximity to the plurality of superhardbearing elements 406 may result in erosion of the support ring 402between the superhard bearing elements 406, which may be undesirable.

To provide for increased erosion resistance of the bearing assembly 400,the support ring structure 401 further includes a plurality of erosionresistant regions exhibiting a higher erosion resistance than thesupport ring 402 and disposed between adjacent superhard bearingelements 406 of the plurality of superhard bearing elements 406. Forexample, as shown in FIG. 4D, the support ring 402 may be configured tocarry a plurality of inserts 418 that each functions as an erosionresistant region. Each of the plurality of inserts 418 may extend atleast partially laterally about a corresponding one of the plurality ofsuperhard bearing elements 406. For example, in the illustratedembodiment, each of the plurality of inserts 418 extends peripherallycompletely about one of the superhard bearing elements 406. Each of theplurality of inserts 418 may comprise an erosion resistant materialexhibiting a higher erosion resistance than the support ring 402. Forexample, the plurality of inserts 418 may comprise a carbide, asuperhard material, a metal carbide (e.g., tungsten carbide, niobiumcarbide, molybdenum carbide, vanadium carbide, titanium carbide, orcombinations thereof), a cemented carbide (e.g., tungsten carbide,niobium carbide, molybdenum carbide, boron carbide, silicon carbide,vanadium carbide, titanium carbide, or combinations thereof cementedwith cobalt, iron, nickel, or alloys thereof), diamond, boron nitride,combinations of the foregoing, or other suitable erosion resistantmaterial. The plurality of inserts 418 may be pre-machined to tolerancesand mounted to the support ring 402 via brazing, interference-fitted,press-fitting, threadly attaching, fastening with a fastener,combinations of the foregoing, or another suitable technique.

The annular slot 423 receives the plurality of inserts 418 and each ofthe plurality of inserts 418 receives a corresponding one of theplurality of superhard bearing elements 406. Each of the plurality ofinserts 418 may include a hole 420 therein (shown in FIG. 4E) throughwhich a corresponding one of the superhard bearing elements 406projects. The positioning of the superhard bearing elements 406 into theholes 420 of the inserts 418 provides for erosion resistant regionssurrounding each of the superhard bearing elements 406.

Similar to the superhard bearing elements 110, the superhard bearingelements 406 may be machined to tolerances and mounted in the holes 420of the inserts 418 and the support ring 402. Bearing surfaces 412 may beplanarized (e.g., by lapping and/or grinding) and/or positioned so thatthe bearing surfaces 412 are substantially coplanar with each other.Optionally, one or more of the superhard bearing elements 406 mayexhibit a peripherally extending edge chamfer 424 (shown in FIG. 4B-4D).However, in other embodiments, the edge chamfer 424 may be omitted ormay extend partially along one or more selected portions of theperiphery of bearing surface 412.

Embodiments of the invention may include inserts of varying suitableshapes and configurations. For example, a cross-sectional shape of theinserts may exhibit a round, square, polygonal, oval, rectangular, orother suitable shape that may include a hole or recess for receiving atleast a portion of a superhard bearing element. FIGS. 5A, 5B, 6A and 6Billustrate two embodiments each with a varied shape of insert forreceiving superhard bearing elements 510 and 610.

FIGS. 5A and 5B are isometric views of a thrust-bearing assembly 500 andan insert 502, respectively, according to one or more embodiments. Theplurality of inserts 502 shown in FIGS. 5A and 5B may each be receivedby an annular slot 504 formed within a support ring 506 to define asupport ring structure 507. The plurality of inserts 502 may begenerally rectangular shaped and include two semi-circular recesses 508(e.g., cutouts) on opposite sides of the insert 502, as shown in FIG.5B. Each of the recesses 508 is configured to receive a portion ofsuperhard bearing element 510 such that one superhard bearing element510 is positioned with a recess 508 on each side of the superhardbearing element 510, as shown in FIG. 5A. Such a configuration mayprovide a substantially continuous erosion resistant region surroundinga periphery of each of the plurality of superhard bearing elements 510.

FIGS. 6A and 6B are isometric views of a thrust-bearing assembly 600 andan insert 602, respectively, according to one or more embodiments. Eachof the plurality of inserts 602 shown in FIGS. 6A and 6B may be receivedby an annular slot 604 formed within a support ring 606 to define asupport ring structure 607. Each of the plurality of inserts 602 may begenerally rectangular shaped and include two arcuate recesses 608 onopposite sides of the insert 602. Similar to the inserts 502 andsemi-circular recesses 508 of FIGS. 5A and 5B, each of the recesses 608is configured to receive a superhard bearing element 610 such that oneof the superhard bearing elements 610 is positioned with recesses 608 oneach side thereof for providing an erosion resistant region surroundinga periphery of each of the plurality of superhard bearing elements 610.

Any of the thrust-bearing assembly embodiments disclosed herein may beemployed in a thrust-bearing apparatus. For example, FIGS. 7A and 7Billustrate a thrust-bearing apparatus 700 according to an embodiment.The thrust-bearing apparatus 700 may include a stator 702 as shown inFIG. 7A. The stator 702 may include a support ring structure 704including an erosion resistant coating 706 (shown in FIG. 7B) formed ona support ring 708. A plurality of superhard bearing elements 710 aremounted to the support ring 708. The thrust-bearing apparatus 700further may include a rotor 712. The rotor 712 may include a supportring structure 714 including an erosion resistant coating 716 (shown inFIG. 7B) formed on a support ring 718 and a plurality of superhardbearing elements 720 mounted or otherwise attached within acorresponding plurality of recesses 722 of the support ring 718. Ofcourse, the stator 702 or rotor 712 may be configured according to anyof the other embodiments disclosed herein. In an embodiment, only one ofthe stator 702 or rotor 712 may include erosion resistant regions,erosion resistant inserts, or erosion resistant coatings as describedherein. For example, in an embodiment only one of the rotor 712 orstator 702 may include the erosion resistant coating 706 and the erosionresistant coating 716. It is noted that in other embodiments, the rotoror stator may be configured as any of the previously describedembodiments of thrust-bearing assemblies.

As shown in FIG. 7A, a shaft 722 may be coupled to the support ring 718and operably coupled to an apparatus capable of rotating the shaft 722in a direction R (or in a generally opposite direction), such as adownhole motor. For example, the shaft 722 may extend through and may besecured to the support ring 718 of the rotor 712 by press-fitting orthreadly coupling the shaft 722 to the support ring 718 or anothersuitable technique. A housing 724 may be secured to a support ring 708of the stator 702 and may extend circumferentially about the shaft 722and the rotor 712.

The concepts used in the thrust-bearing assemblies and apparatusesdescribed above may also be employed in radial bearing assemblies andapparatuses. For example, FIGS. 8A-8C are isometric exploded cutaway,isometric, and isometric cutaway views, respectively, of a radialbearing apparatus 800 according to an embodiment. The radial bearingapparatus 800 may include a first radial bearing assembly 802 (i.e., aninner race) and a second radial bearing assembly 804 (i.e., an outerrace). The first radial bearing assembly 802 may be configured as arotor and may include a support ring structure 805 including a supportring 806 and a plurality of superhard bearing elements 808 extendingabout a rotation axis 810. The support ring 806 may include an innerperipheral surface defining a central opening 812.

As shown in FIG. 8A, the support ring structure 805 includes the supportring 806 and may be configured with an annular slot 818 to carry aplurality of inserts 814 that may enhance the erosion resistance of thesupport ring 806. The plurality of inserts 814 may comprise a carbide, asuperhard material, a metal carbide (e.g., tungsten carbide, niobiumcarbide, molybdenum carbide, vanadium carbide, titanium carbide, orcombinations thereof), a cemented carbide (e.g., tungsten carbide,niobium carbide, molybdenum carbide, boron carbide, silicon carbide,vanadium carbide, titanium carbide, or combinations thereof cementedwith cobalt, iron, nickel, or alloys thereof), diamond, boron nitride,combinations of the foregoing, or other suitable erosion resistantmaterial. The plurality of inserts 814 may be pre-machined to tolerancesand mounted in the annular slot 818 of the support ring 806 via brazing,press-fitting, threadly attaching, fastening with a fastener,combinations of the foregoing, or another suitable technique. Each ofthe plurality of inserts 814 may include a hole 816 (shown in FIG. 8C)for receiving a corresponding one of the superhard bearing elements 808.According to various embodiments, the inserts 814 may exhibit varioussuitable shapes and configurations. For example, the inserts 814 mayexhibit a round, square, polygonal, oval, rectangular, or other suitableshape that may include a through or blind hole for receiving a superhardbearing element 808.

As illustrated in FIG. 8A, the superhard bearing elements 808 may bedistributed circumferentially about the rotation axis 810 incorresponding holes 816 and within the annular slot 818 formed in thesupport ring 806 of the support ring structure 805 and arranged in asingle row. In other embodiments, the superhard bearing elements 808 maybe circumferentially distributed in two rows, three rows, four rows, orany other number of rows. At least one, some of, or each superhardbearing element 808 may include a superhard table 820 (shown in FIG. 8A)including a convexly-curved bearing surface 822 (e.g., curved to lie onan imaginary cylindrical surface). Each superhard table 820 may bebonded or attached to a corresponding substrate 824. The superhardbearing elements 808 may have generally cylindrical shaped bodies andmay be made from any of the materials discussed above for the superhardbearing elements 110, 206, 510 or 610. In other embodiments, thesuperhard bearing elements 808 may have different shapes and/or sizes.For example, one or more of the superhard bearing surfaces 822 may havea generally rounded rectangular shaped surface, a generally ellipticalshaped surface, a generally wedge shaped surface, a generally polygonalshaped surface, or any other suitable shaped surface and/or at least oneof the superhard bearing elements 808 may be sized larger than anotherone of the superhard bearing elements 808.

The second radial bearing assembly 804 may be configured as a statorthat extends about and receives the first radial bearing assembly 802(i.e., rotor). The second radial bearing assembly 804 may be generallyconfigured similar to the first radial bearing assembly 802 or any otherradial bearing assembly disclosed herein. For example, the second radialbearing assembly 804 may include a support ring structure 825 comprisinga support ring 826 including an annular slot 832 (FIG. 8C), a pluralityof inserts 828 formed from any of the materials disclosed herein for theinserts 814, and a plurality of superhard bearing elements 830. Theplurality of inserts 828 and the superhard bearing elements 830 may bedistributed circumferentially about the rotation axis 810 within theannular slot 832 (shown in FIGS. 8C and 8D) formed in the support ring826. As illustrated in FIGS. 8C and 8E, each of the plurality of inserts828 may include a hole 816. Each of the plurality of inserts 828receives a corresponding one of the plurality of superhard bearingelements 830.

The positioning of the superhard bearing elements 830 into the holes 816of the inserts 828 may provide erosion resistance regions laterallysurrounding each of the superhard bearing elements 830. The superhardbearing elements 830 may be machined to tolerances and mounted in theholes 816 of the inserts 828 and annular slot 832 of the support ring826 and/or attached to the support ring 826 of the support ringstructure 825 according to any of the embodiments disclosed herein.

At least one of, some of, or each superhard bearing element 830 mayinclude a superhard table 834 (shown in FIG. 8C) including aconcavely-curved bearing surface 836 curved to correspond to theconvexly-curved bearing surfaces 822 of the superhard bearing elements808. Each of the superhard bearing elements 830 including the concavelycurved bearing surface 836 may be oriented to engage the convexly-curvedbearing surfaces 822 of the first bearing assembly 802 during operation.Similar to the superhard bearing elements 808, the superhard bearingelements 830 may have generally cylindrical shaped bodies and may bemade from any of the materials and structures discussed above for any ofthe superhard bearing elements disclosed herein.

While the superhard bearing elements 830 are shown configured similarlyto one another and the superhard bearing elements 808, in otherembodiments, the superhard bearing elements 830 may have shapes and/orsizes that vary from one another and/or the superhard bearing elements808. For example, one or more of the superhard bearing elements 830 mayhave any solid geometry such as a generally cubic geometry, a generallypolyhedron geometry, or any generally plane geometry that has athickness or depth. For example, a bearing surface 836 of a superhardbearing element 830 may have a generally rectangular shape, a generallyelliptical shape, a generally wedge shape, a generally polygonal shape,a generally oval shape, or any other suitable geometry. In otherembodiments, at least one of the superhard bearing elements 808 may havea generally rectangular shape and at least one of the superhard bearing830 elements may have a generally elliptical shape. In yet otherembodiments, at least one of the superhard bearing elements 830 may besized larger than at least one of the superhard bearing elements 808.

In an embodiment, a shaft or spindle (not shown) may extend through theopening 812 and may be secured to the first radial bearing assembly 802,threadly coupling the shaft or spindle to the first radial bearingassembly 802, or another suitable technique. A housing (not shown) mayalso be secured to the second radial bearing assembly 804 using similartechniques. While the first radial bearing assembly 802 is shownconfigured as the rotor and the second radial bearing assembly 804 isshown configured as the stator, in other embodiments, the first radialbearing assembly 802 may be configured as the stator and the secondradial bearing assembly 804 may be configured as the rotor.

FIGS. 9A and 9B are isometric and isometric cutaway views, respectively,of a thrust-bearing assembly 900 according to an embodiment. Thethrust-bearing assembly 900 may form a stator or a rotor of athrust-bearing apparatus such as the thrust-bearing apparatus 700 shownin FIGS. 7A and 7B. As shown in FIGS. 9A and 9B, the thrust-bearingassembly 900 may include a support ring structure 901 including asupport ring 902 defining an opening 904 through which a shaft (notshown) of, for example, a downhole drilling motor may extend. Thesupport ring 902 may be made from a variety of different materials. Forexample, the support ring 902 may comprise a metal, an alloy steel, ametal alloy, carbon steel, a stainless steel, tungsten carbide, anyother suitable conductive or non-conductive material, combinations ofthe foregoing, or any material disclosed herein.

The thrust-bearing assembly 900 may include a plurality of superhardbearing elements 906. Each of the plurality of superhard bearingelements 906 may comprise a superhard compact such as a polycrystallinediamond compact. In an embodiment, one or more of the superhard bearingelements 906 may have a general wedge shape. In other embodiments, oneor more of the superhard bearing elements 906 may have any solidgeometry such as a generally cubic geometry, a generally polyhedrongeometry, or any generally plane geometry that has a thickness or depth.

For example, a bearing surface of the superhard bearing element 906 mayhave a generally 2D rectangular shape, a generally cylindrical shape, agenerally oval shape, a generally polygonal shape, or any other suitablegeometry.

The superhard bearing elements 906 may include a superhard table 908bonded to a substrate 910, and a bearing surface 912 of the superhardtable 908 (shown in FIG. 9C and FIG. 9E). The substrate 910 may extendat least partially laterally about one of the plurality of superhardbearing elements 906 to form lateral extensions 914. For example, asshown in FIG. 9A-9C, the lateral extensions 914 extend laterally abouteach of the plurality of superhard bearing elements 906. The lateralextensions 914 may be comprised of a carbide, a superhard material, ametal carbide (e.g., tungsten carbide, niobium carbide, molybdenumcarbide, vanadium carbide, titanium carbide, or combinations thereof), acemented carbide (e.g., tungsten carbide, niobium carbide, molybdenumcarbide, diamond, boron carbide, silicon carbide, boron nitride,vanadium carbide, titanium carbide, or combinations thereof cementedwith cobalt, iron, nickel, or alloys thereof), or other suitable erosionresistant material to provide for greater erosion resistance of thesupport ring 902. For example, the lateral extensions 914 may provideenhanced erosion resistance of the support ring 902 during operation ofthe thrust-bearing assembly 900.

The superhard bearing elements 906 are illustrated in FIG. 9A beingdistributed circumferentially about a thrust axis 916 along which athrust force may be generally directed during use. The superhard bearingelements 906 may be circumferentially distributed about the thrust axis916 in one row, two rows, three rows, or any number of suitable rows. Asshown, gaps 918 may be located between adjacent ones of the superhardbearing elements 906. In an embodiment, at least one of, some of, or allof the gaps 918 may exhibit width of about 0.00020 inches to 0.500inches, such as about 0.10 inches to about 0.3 inches, about 0.10 inchesto about 0.4 inches, about 0.00040 inches to 0.0010 inches, or about0.00040 inches to 0.080 inches. In other embodiments, the gaps 918 mayhave widths that are relatively larger or smaller. In other embodiments,the gaps 918 may substantially be zero. In other embodiments, one ormore of the gaps 918 may have different widths. For example, one pair ofadjacent ones of the superhard bearing elements 906 may be closertogether than another pair of adjacent ones of the superhard bearingelements 906.

As shown in FIG. 9B, the support ring structure 901 including thesupport ring 902 carries the plurality of superhard bearing elements906, with each of the plurality of superhard bearing elements 906including the two lateral extensions 914, one lateral extension 914 oneach side of each of the plurality of superhard bearing elements 906.

Each of the plurality of superhard bearing elements 906 andcorresponding extensions 914 may be partially disposed within an annularslot 920 (shown in FIG. 9B) of the support ring 902 of the support ringstructure 901. The positioning of the superhard bearing elements 906 andcorresponding lateral extensions 914 into the annular slot 920 of thesupport ring 902 may provide erosion resistant regions laterallysurrounding each of the superhard bearing elements 906. The superhardbearing elements 906 and corresponding extensions 914 may bepre-machined to tolerances and mounted into the annular slot 920 of thesupport ring 902 of the support ring structure 901 as described withreference to superhard bearing elements 110 or as otherwise describedherein. Bearing surfaces 912 may be planarized (e.g., by lapping and/orgrinding) and/or positioned so that the bearing surfaces 912 aresubstantially coplanar. Optionally, one or more of the superhard bearingelements 906 may exhibit a peripherally extending edge chamfer 920(shown in FIG. 9B-9E). However, in other embodiments, the edge chamfer920 may be omitted.

According to an embodiment, the plurality of superhard bearing elements906 and corresponding extensions 914 may be cut from a generallycylindrical superhard compact. For example, as shown in FIG. 9D, thesuperhard table 908 of a cylindrical superhard compact 922 may be cutand shaped using wire electrical discharge machining (“EDM”), lasermachining, or any other suitable method so that portions of thesubstrate 910 are exposed that define the lateral extensions 914.

The concepts used in the thrust-bearing assemblies and apparatusesdescribed above may also be employed in radial bearing assemblies andapparatuses. FIG. 10 is an isometric view illustrating a radial bearingassembly 1000 according to an embodiment. The radial bearing assembly1000 may include a support ring structure 1001 including a support ring1002 extending about a rotation axis 1016. The support ring 1002 mayinclude a central opening 1004 that is capable of receiving, forexample, an inner support ring or inner race. A plurality of superhardbearing elements 1008 may be distributed circumferentially about therotation axis 1016. Each superhard bearing element 1008 may include asuperhard table 1010 including a concavely-curved bearing surface 1014(e.g., curved to lie on an imaginary cylindrical surface). Eachsuperhard table 1010 may be bonded or attached to a correspondingsubstrate. The superhard bearing elements 1008 may have a generallyrectangular shape and each made from any of the materials discussedabove for the superhard bearing elements 110. In other embodiments, thesuperhard bearing elements 1008 may have a non-rectangular shape, ageneral wedge-like shape, a general cylindrical shape, a generallypolygonal shape, or any other suitable geometry. As illustrated in FIG.10, the superhard bearing elements 1008 may be distributedcircumferentially about the rotation axis 1016 in an annular slot (notshown) formed in the support ring 1002 of the support ring structure1001 and arranged in a single row. In other embodiments, the superhardbearing elements 1008 may be circumferentially distributed in two rows,three rows, four rows, or any number of rows.

The radial bearing assembly 1000 described above may be used as a rotoror stator in a bearing apparatus that may be employed in a variety ofmechanical applications. For example, so-called “rotary cone” rotarydrill bits, pumps, transmissions or turbines may benefit from a radialbearing apparatus discussed herein.

FIG. 11 is a schematic isometric cutaway view of a subterranean drillingsystem 1100 according to an embodiment. The subterranean drilling system1100 may include a housing 1136 enclosing a downhole drilling motor 1138(i.e., a motor, turbine, or any other device capable of rotating anoutput shaft) that may be operably connected to an output shaft 1140. Athrust-bearing apparatus 1142 may be operably coupled to the downholedrilling motor 1138. The thrust-bearing apparatus 1142 may be configuredas any of the previously described thrust-bearing apparatus embodiments.A rotary drill bit 1144 may be configured to engage a subterraneanformation and drill a borehole and may be connected to the output shaft1140. The rotary drill bit 1144 is shown comprising a bit body 1146 thatincludes radially-extending and longitudinally-extending blades 1148with a plurality of polycrystalline diamond compacts 1150 secured to theblades 1148. However, other embodiments may utilize different types ofrotary drill bits, such as so-called core bits, or roller-cone bits. Asthe borehole is drilled, pipe sections may be connected to thesubterranean drilling system 1100 to form a drill string capable ofprogressively drilling the borehole to a greater depth within the earth.

The thrust-bearing apparatus 1142 may include a stator 1152 that doesnot rotate and a rotor 1154 that may be attached to the output shaft1140 and rotates with the output shaft 1140. As discussed above, thethrust-bearing apparatus 1142 may be configured as any of theembodiments disclosed herein. For example, the stator 1152 and the rotor1154 may include a plurality of circumferentially-distributed superhardbearing elements (not shown) similar to those shown and described inrelation to FIG. 1. In operation, lubricating fluid may be circulatedthrough the downhole drilling motor 1138 to generate torque and rotatethe output shaft 1140 and the rotary drill bit 1144 attached thereto sothat a borehole may be drilled. A portion of the lubricating fluid mayalso be used to lubricate opposing bearing surfaces of the stator 1152and the rotor 1154.

Although the bearing assemblies and apparatuses described above havebeen discussed in the context of subterranean drilling systems andapplications, in other embodiments, the bearing assemblies andapparatuses disclosed herein are not limited to such use and may be usedfor many different applications, if desired, without limitation. Thus,such bearing assemblies and apparatuses are not limited for use withsubterranean drilling systems and may be used with various mechanicalsystems, without limitation.

While various aspects and embodiments have been disclosed herein, otheraspects and embodiments are contemplated. The various aspects andembodiments disclosed herein are for purposes of illustration and arenot intended to be limiting. Additionally, the words “including,”“having,” and variants thereof (e.g., “includes” and “has”) as usedherein, including the claims, shall be open ended and have the samemeaning as the word “comprising” and variants thereof (e.g., “comprise”and “comprises”).

What is claimed is:
 1. A method of fabricating a bearing assembly, themethod comprising: providing a support ring that includes a plurality ofrecesses and/or an annular slot, the plurality of recesses and/or theannular slot extending from an upper surface of the support ring onlypartially through the support ring to a lower surface of the pluralityof recesses and/or the annular slot; mounting a plurality of superhardbearing elements to the support ring, each of the plurality of superhardbearing elements exhibiting a generally uniform cross-sectional widthalong a depth of the plurality of recesses and/or the annular slot fromthe upper surface to the lower surface; and disposing at least oneerosion resistant region on a portion of the support ring, the at leastone erosion resistant region exhibiting an erosion resistance that isgreater than the support ring; wherein the at least one erosionresistant region is at least one of: formed only on as the upper surfaceof the support ring, positioned in the annular slot, or spaced from atleast one adjacent superhard bearing element of the plurality ofsuperhard bearing elements.
 2. The method of claim 1 wherein: thesupport ring includes the annular slot having a base surface and twoopposing sidewalls; and disposing at least one erosion resistant regionon a portion of the support ring includes securing at least one erosionresistant insert in the annular slot.
 3. The method of claim 1 wherein:mounting the plurality of superhard bearing elements to the support ringincludes disposing at least a portion of the plurality of superhardbearing elements in a corresponding one of the plurality of recesses;and disposing at least one erosion resistant region on a portion of thesupport ring includes depositing an erosion resistant coating on theportion of the support ring.
 4. The method of claim 3 wherein depositingan erosion resistant coating on the portion of the support ring isperformed before mounting a plurality of superhard bearing elements tothe support ring.
 5. The method of claim 4 wherein depositing an erosionresistant coating on the portion of the support ring includes depositingthe erosion resistant coating on at least one of the plurality ofrecesses.
 6. The method of claim 3 wherein depositing an erosionresistant coating on the portion of the support ring is performed aftermounting a plurality of superhard bearing elements to the support ring.7. The method of claim 6 wherein depositing an erosion resistant coatingon the portion of the support ring includes depositing the erosionresistant coating on a region of the support ring that iscircumferentially between the plurality of superhard bearing elementsand is spaced from at least one adjacent superhard bearing element ofthe plurality of superhard bearing elements by about 5 μm to about 6.4mm.
 8. The method of claim 6, further comprising, before depositing anerosion resistant coating on the portion of the support ring,positioning protective cups over at least one of the plurality ofsuperhard bearing elements.
 9. The method of claim 3 wherein depositingan erosion resistant coating on the portion of the support ring includesdepositing the erosion resistant coating by chemical vapor deposition.10. The method of claim 3 wherein depositing an erosion resistantcoating on the portion of the support ring includes depositing theerosion resistant coating by at least one of laser-deposition, physicalvapor deposition, thermal spray deposition, or a high-velocity oxygenfuel thermal spray process.
 11. The method of claim 3 wherein mounting aplurality of superhard bearing elements to the support ring includesbrazing the plurality of superhard bearing elements to the support ring.12. The method of claim 3 wherein depositing an erosion resistantcoating on the portion of the support ring includes: providing apreformed erosion resistant coating; and brazing or welding thepreformed erosion resistant coating to the portion of the support ring.13. The method of claim 12 wherein brazing or welding the preformederosion resistant coating to the portions of the support ring compriseswelding the preformed erosion resistant coating to the portion of thesupport ring with tungsten inert gas welding, metal arc welding, orplasma transferred arc welding.
 14. The method of claim 3, furthercomprising, after depositing an erosion resistant coating on the portionof the support ring, machining the erosion resistant coating.
 15. Amethod of fabricating a bearing assembly, the method comprising:providing a support ring that includes a plurality of recesses, each ofthe plurality of recesses are defined by at least one recess surface,the plurality of recesses extending only partially through the supportring; positioning a plurality of superhard bearing elements such thateach of the plurality of superhard bearing elements is positioned in acorresponding one of the plurality of recesses of the support ring, eachof the plurality of superhard bearing elements exhibiting a generallyuniform transverse cross-sectional shape along a height of each of theplurality of superhard bearing elements; and laser depositing at leastone erosion resistant coating only on an upper surface of the supportring, the erosion resistant coating exhibiting an erosion resistancethat is greater than the support ring and includes at least one of asuperhard material, a metal carbide, or a cemented carbide.
 16. Themethod of claim 15 wherein laser depositing an erosion resistant coatingonly on an upper surface of the support ring is performed beforemounting a plurality of superhard bearing elements to the support ring.17. The method of claim 15 wherein laser depositing an erosion resistantcoating only on an upper surface of the support ring is performed aftermounting a plurality of superhard bearing elements to the support ring.18. The method of claim 17 wherein laser depositing an erosion resistantcoating only on an upper surface of the support ring includes depositingthe erosion resistant coating on a region of the support ring that iscircumferentially between the plurality of superhard bearing elementsand is spaced from the at least one adjacent superhard bearing elementof the plurality of superhard bearing elements by about 5 μm to about6.4 mm.
 19. The method of claim 15, further comprising brazing at leastone of the plurality of superhard bearing elements to the support ring.20. A method of fabricating a bearing assembly, the method comprising:providing a support ring that includes a plurality of recesses;positioning a plurality of superhard bearing elements such that each ofthe plurality of superhard bearing elements is positioned in acorresponding one of the plurality of recesses of the support ring, eachof the plurality of superhard bearing elements exhibiting a generallyuniform transverse cross-sectional shape along a height of each of theplurality of superhard bearing elements; and forming at least oneerosion resistant coating on a portion of the support ring so that theerosion resistant coating is spaced from at least one adjacent superhardbearing element of the plurality of superhard bearing elements by about5 μm to about 6.4 mm; wherein the erosion resistant coating exhibitingan erosion resistance that is greater than the support ring; wherein theerosion resistant coating includes at least one of a superhard material,a metal carbide, or a cemented carbide.